An Analytical procedure for computing smooth transitions between two specified cross sections with applications to blended wing-body configurations
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Author
Contributions
- Langley Research Center - Contributor
- United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch - Contributor
Publication
1982 - For sale by the National Technical Information Service], Washington, D.C, District of Columbia
Language
English
Subjects
Series Statement
- NASA technical paper -- 2012
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